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ArtScience4 months ago

Inter-stellar spacecraft are powered by an electro-dynamic high frequency polarizing centravac attenuation vortex assembly. The non-ferritic hydromagnetic reaction fluid is hydrodynamically down-converted using an isotopic impedance-driven ion separation cavity where it is semi-centrifugally divided into equal positive and negative anti-trons. The  re-polarized anti-positive pro-neutrons are transmitted through triaxial multi-helix hydronic wave guides and directed by poly-convex triple-dipole parabolic klysro-magnetic attenuation antennas. The induced ultra-high induction gamma reaction field causes non-charged electron groups to simultaneously de-couple. The negative ion anti-pro neutron force field effect is inductively modulated and fed to multi-cyclic paralleling transducer modules oscillating in at a harmonic pulse which is non- plussed at 180 degrees and phase loaded. The synchronous rotron micro-absorber fluid is transmoginated and magnetically down-sorted by ion drive flux capacitors and directed to parallel beam parabolic back-feed antennas which are auto-gyrated on pivotal hyperbolic, reverse-aperture sphere nozzles.

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